CA2308131A1 - Mecanisme de commande d'ejection pour tuyeres convergentes-divergentes - Google Patents

Mecanisme de commande d'ejection pour tuyeres convergentes-divergentes Download PDF

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Publication number
CA2308131A1
CA2308131A1 CA002308131A CA2308131A CA2308131A1 CA 2308131 A1 CA2308131 A1 CA 2308131A1 CA 002308131 A CA002308131 A CA 002308131A CA 2308131 A CA2308131 A CA 2308131A CA 2308131 A1 CA2308131 A1 CA 2308131A1
Authority
CA
Canada
Prior art keywords
exit area
group
control mechanism
area control
divergent nozzles
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CA002308131A
Other languages
English (en)
Other versions
CA2308131C (fr
Inventor
Javier Elorriaga Vicario
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Industria de Turbo Propulsores SA
Original Assignee
Industria De Turbo Propulsores, S.A.
Javier Elorriaga Vicario
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Industria De Turbo Propulsores, S.A., Javier Elorriaga Vicario filed Critical Industria De Turbo Propulsores, S.A.
Publication of CA2308131A1 publication Critical patent/CA2308131A1/fr
Application granted granted Critical
Publication of CA2308131C publication Critical patent/CA2308131C/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/15—Control or regulation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • F02K1/008—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector in any rearward direction
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1223—Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/32—Arrangement of components according to their shape
    • F05D2250/323—Arrangement of components according to their shape convergent
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/32—Arrangement of components according to their shape
    • F05D2250/324—Arrangement of components according to their shape divergent

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Jet Pumps And Other Pumps (AREA)
CA002308131A 1999-05-13 2000-05-12 Mecanisme de commande d'ejection pour tuyeres convergentes-divergentes Expired - Fee Related CA2308131C (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP99500079.1 1999-05-13
EP99500079A EP1052395B1 (fr) 1999-05-13 1999-05-13 Dispositif de commande de la section de sortie d'une tuyère convergente-divergente

Publications (2)

Publication Number Publication Date
CA2308131A1 true CA2308131A1 (fr) 2000-11-13
CA2308131C CA2308131C (fr) 2009-02-03

Family

ID=8242498

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002308131A Expired - Fee Related CA2308131C (fr) 1999-05-13 2000-05-12 Mecanisme de commande d'ejection pour tuyeres convergentes-divergentes

Country Status (5)

Country Link
US (1) US6378781B1 (fr)
EP (1) EP1052395B1 (fr)
CA (1) CA2308131C (fr)
DE (1) DE69918531T2 (fr)
ES (1) ES2224580T3 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140298772A1 (en) * 2013-04-04 2014-10-09 MTU Aero Engines AG Mischvorrichtung und turbofantriebwerk mit einer derartigen mischvorrichtung

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7721551B2 (en) * 2006-06-29 2010-05-25 United Technologies Corporation Fan variable area nozzle for a gas turbine engine fan nacelle
WO2008045069A1 (fr) * 2006-10-12 2008-04-17 United Technologies Corporation Tuyère à section variable à soufflante avec actionneur électromécanique
US8549834B2 (en) 2010-10-21 2013-10-08 United Technologies Corporation Gas turbine engine with variable area fan nozzle
US8783605B2 (en) * 2010-12-28 2014-07-22 Rolls-Royce North American Technologies, Inc. Flight vehicle, propulsion system and thrust vectoring system
EP2971724B1 (fr) 2013-03-13 2020-05-06 Rolls-Royce North American Technologies, Inc. Système d'actionnement compact pour tuyère d'échappement de moteur de turbine à gaz
RU2535516C1 (ru) * 2013-04-11 2014-12-10 Открытое акционерное общество "Уфимское моторостроительное призводственное объединение" ОАО "УМПО" Регулируемое сопло турбореактивного двигателя
US10371089B2 (en) * 2015-01-20 2019-08-06 United Technologies Corporation System for actuating an exhaust cowl
CN107029911A (zh) * 2017-06-05 2017-08-11 盐城东方天成机械有限公司 一种手动静电粉末喷枪
CN111322912A (zh) * 2020-03-06 2020-06-23 南京理工大学 一种滚珠丝杠协同驱动的推力矢量全轴摆动喷管
CN113374594B (zh) * 2021-06-21 2022-12-20 中国航发沈阳发动机研究所 一种二元喷管扩张段控制机构
CN114776468A (zh) * 2022-04-14 2022-07-22 中国航发沈阳发动机研究所 一种轴对称收扩喷管双环控制机构

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2811831A (en) * 1951-06-29 1957-11-05 United Aircraft Corp Variable area nozzle
DE2809169C3 (de) * 1978-03-03 1980-11-27 Mtu Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Strahlrohr zum Antrieb und zur Steuerung von Flugzeugen
KR0167796B1 (ko) * 1990-08-23 1998-12-15 존 스와토챠 짐블드 유니즌 링이 구비된 축대칭 노즐
ES2136528B1 (es) * 1996-12-26 2000-05-01 Sener Ing & Sist Perfeccionamientos en toberas axisimetricas de geometria variable y orientacion del flujo destinadasa propulsores de turbina de gas
DE69719482T2 (de) * 1997-01-23 2004-03-18 Industria De Turbo Propulsores S.A., Zamudio Divergierende Düsenklappe für die Düse eines Gasturbinentriebwerks
ES2208850T3 (es) * 1997-06-16 2004-06-16 Industria De Turbo Propulsores, S.A. Conjunto de montaje para un petalo principal divergente de una tobera de geometria variable.

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140298772A1 (en) * 2013-04-04 2014-10-09 MTU Aero Engines AG Mischvorrichtung und turbofantriebwerk mit einer derartigen mischvorrichtung
US9771896B2 (en) * 2013-04-04 2017-09-26 MTU Aero Engines AG Mixing device and turbofan engine having such mixing device

Also Published As

Publication number Publication date
EP1052395B1 (fr) 2004-07-07
EP1052395A1 (fr) 2000-11-15
DE69918531T2 (de) 2005-08-18
ES2224580T3 (es) 2005-03-01
US6378781B1 (en) 2002-04-30
CA2308131C (fr) 2009-02-03
DE69918531D1 (de) 2004-08-12

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Effective date: 20180514